ELECTRON R/B (1), 68800 (Decayed)
Orbit data source: Space-Track
ELECTRON R/B (1), 68800 was space debris in LEO originally from a launch on Thu, 23 Apr 2026 UTC launched from the Rocket Lab Launch Complex (RLLC). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
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68800 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Rocket Lab
Mission
Decayed spacecraft
Bus & Motor
ELECTRON ST2, Unknown motor
Mass
250 kg wet, ~250 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 8.0 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 months ago
TLE from 2 months ago
0 ELECTRON R/B (1)
1 68800U 26088J 26122.86562641 .06289310 21116-5 77176-3 0 9993
2 68800 97.4658 274.5343 0096649 180.4728 179.6487 16.21182415 1548Epoch: 2026-05-02T20:46Z
TLE epoch observation values (Epoch: 2026-05-02T20:46:30.121Z)
Latitude
-0.00006°
Longitude
102.13141°
Altitude
283.317 km
Speed
7.7 km/s
True Right ascension
18h 18m 08s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
08:42:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
276.882 km
Perigee altitude
149.474 km
Semi-major axis
6,591.315 km
Eccentricity
0.00966
Inclination
97.4658°
RAAN
274.5343°
Arg. of periapsis
180.4728°
True anomaly
179.65541°
Mean anomaly
179.6487°
Eccentric anomaly
179.65206°
Mean motion
4.05588 °/min
Orbital period
88.76 mins
BSTAR
0.00077176
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Other satellites on launch #88 in the year 2026 (2026-04-23 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.ELECTRON R/B (1) Visibility
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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| This satellite is decayed. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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